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FIVE QUESTIONS ANSWER ALL Question 1 A cylindrical specimen of Aluminum having a diameter of 12.8 mm and a gauge length of 50.800 mm is pulled in tension. Use the load-elongation characteristics shown in the following table to complete Q1(a) through (f). Raw Data Load (N) Length (mm) 50.800 7330 50.851 15100 50.902 23100 50.952 30400 51.003 34400 51.054 38400 51.308 41300 51.816 44800 52.832 46200 53.848 47300 54.864 47500 55.880 46100 56.896 44800 57.658 42600 58.420 36400 59.182 a) Plot both the engineering stress versus engineering strain and true stress versus true strain curves on the same axis. EV[8] b) Compute the modulus of elasticity. EV[3] c) Determine the yield strength at a strain offset of 0.002. AN[3] d) Determine the tensile strength of this alloy. AN[2] e) Compute the modulus of resilience. AN[2] f) What is the ductility, in percent elongation? AN[2]

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ed Mar 17 ELEC 110 90-Degree Bends Worksheet copy Home Insert Draw Layout Review View ramond 14 A.. A E E E E A ELEC TIO 90° Bends Worksheet Overview Follow the directions to fill-in the missing values in the tables below. Assignment Determine the take-up and measurement to your mark for each of the following. Length EMT Size Take-up Stub-up Height Mark 70" 1/" 1' – 3" 70" 1" 2' – 0" 70" 16" 70" 1'/," 3' – 2" 70" 1' – 10" Determine the missing values for each of the back-to-back bends below. S2 Gain 71" 10" 15"

Explain the concept of 1x1 convolutions and how it can be used?

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State the main constituent elements of electrical cables, as well as the materials from which they may be made. Describe the following designations: H05VV-U 1G4 mm? and LSXAV 3x16 mm?.

Identify each characteristic curve by the type of FET that it represents. Ip +VGs -VGS

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Problem 1.11 A large steel plate under uniform applied tensile stress contains two cracks, both of which are remote from the edges of the plate and from each other. One is 12 mm in length and is inclined at an angle a= 30°, the other is 15 mm in length and is inclined at an angle B= 45° (figure 1.15). The steel has fracture toughness of Kie = 23 MPa/m and Ke=15 MPa/m. a) Calculate the fracture stress of the plate and state which of the two cracks will cause failure and in which failure mode. (1) པ། Figure 1.15: Finite width thin plate under uniform applied smile stress with two cracks

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